The disclosure relates generally to the field of packaging structures, and more particularly, to stress relief structures for reducing warpage in package assemblies.
Modern integrated circuits are formed on semiconductor chips. To increase manufacturing throughput and to lower manufacturing costs, the integrated circuits are manufactured in semiconductor wafers, each containing many identical semiconductor chips. After the integrated circuits are manufactured, semiconductor chips are sawed from the wafers and packaged before they can be used.
In typical packaging processes, semiconductor chips or dies are first attached to package substrates. This includes physically securing the semiconductor chips on the package substrates, and connecting bond pads on the semiconductor chips to bond pads on the package substrates. Underfill, which typically comprises epoxy, is used to further secure the bonding. The semiconductor chips may be bonded using either flip-chip bonding or wire bonding.
After the semiconductor chips are bonded onto the package substrates, the solder regions that join the semiconductor chips with the package substrates often suffer from cracking. This is caused by the stress resulting from the difference in coefficients of thermal expansion (CTE) between the package substrates and the semiconductor chips. The difference in CTEs of different layers of the package substrates and the semiconductor chips also results in stresses. The increase in the size of the package substrates and the semiconductor chips results in stress increase. As a result of the increased stresses, the solder cracking becomes more severe and delamination may occur between different layers of the semiconductor chips. Particularly, the delamination is likely to occur between low-k dielectric layers in the semiconductor chips.
Aspects of the present disclosure are best understood from the following detailed description when read with the accompanying figures. It is emphasized that, in accordance with the standard practice in the industry, various features are not drawn to scale. In fact, the dimensions of the various features may be arbitrarily increased or reduced for clarity of discussion.
In the following description, specific details are set forth to provide a thorough understanding of embodiments of the present disclosure. However, one having an ordinary skill in the art will recognize that embodiments of the disclosure can be practiced without these specific details. In some instances, well-known structures and processes are not described in detail to avoid unnecessarily obscuring embodiments of the present disclosure.
Reference throughout this specification to “one embodiment” or “an embodiment” means that a particular feature, structure, or characteristic described in connection with the embodiment is included in at least one embodiment of the present disclosure. Thus, the appearances of the phrases “in one embodiment” or “in an embodiment” in various places throughout this specification are not necessarily all referring to the same embodiment. Furthermore, the particular features, structures, or characteristics may be combined in any suitable manner in one or more embodiments. It should be appreciated that the following figures are not drawn to scale; rather, these figures are merely intended for illustration.
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According to one or more embodiments, stress relief structures 40 may be formed using photolithography, patterning, and etching techniques. Stress relief structures 40 may be disposed on substrate 20 by means of an adhesive material (not shown) and may comprise any material suitable for attaching stress relief structure 40 onto substrate 20, such as epoxies, urethane, polyurethane, silicone elastomers, and the like. According to one embodiment, the bonding of stress relief structures 40 onto substrate 20 includes coating an adhesive material on a surface of substrate 20. According to one or more embodiments, a curing process may then be performed to cure the adhesive material. The adhesive material may also have a good thermal conductivity, for example, greater than about 10 w/m-° C.
Stress relief structure 40 may be formed of a thermally conductive material such as for example, metal, tungsten, aluminum, aluminum alloy, polysilicon, silicide, tantalum, refractory metal, copper, copper alloy, gold, gold alloy, tantalum nitride, titanium, titanium nitride, nickel, compounds thereof, alloys thereof, or combinations thereof. The scope of the present disclosure is not limited to the above-mentioned materials and other materials are also contemplated such as, for example ceramic, solder, or plastic. The materials used for the stress relief structures 40 may be the same throughout the stress relief structures 40 or may vary at different locations in the stress relief structures 40.
According to one or more embodiments, stress relief structures 40 may have good thermal conductivity, which may be greater than about 20 W/m-° C., for example. Alternatively, stress relief structures 40 have a thermal conductivity equal to or greater than the thermal conductivity of silicon. According to some embodiments, stress relief structure 40 includes substantially a same material as either substrate 20 or dies D1, D2, D3, or D4.
According to one or more embodiments, stress relief structure 40 may have irregular or regular shapes, such as, for example a rectangle (
Still referring to
Experiments have been performed to evaluate the effect of the stress relief structures on the stress reduction of the semiconductor package structure.
According to one or more embodiments, the selecting of the placements of the stress relief structures 40 may be performed automatically using a software algorithm. The selecting of the placements using the software algorithm may be performed in accordance with at least one predetermined design rule taking into account the minimum spacing around a particular die. Further, the selecting of the placements using the software algorithm may be performed by a layout tool during a layout process.
One or more embodiments of the present disclosure may provide numerous advantages, including (but not limited to) reducing the stress caused by the difference in coefficients of thermal expansion (CTE) between the package substrate and one or more dies. Teachings of the present disclosure are particularly applicable to large semiconductor package structures where with the increase in the size of the package substrates and the dies, the stress increases. As a result of the increased stresses, the solder cracking becomes more severe and delamination may occur between different layers of the chips. One or more embodiments of the present disclosure help strengthen the semiconductor package structure and helps reduce the likelihood of cracking and peeling. Moreover, one or more embodiments increase the amount of stress a semiconductor package structure can handle. Further, stiffener rings may provide global stress relief to the semiconductor package structure but may not provide adequate local stress relief. Layout of the stress relief structures in one or more embodiments provide for local stress relief and/or warpage control to the semiconductor package structure. Further still, one or more embodiments of the present disclosure improve the output yield and reliability.
It is understood that the stress relief structures 40 described above in conjunction with
The present disclosure has described various exemplary embodiments. According to one embodiment, a semiconductor package structure, comprises a substrate, a die region having one or more dies disposed on the substrate, and at least one stress relief structure disposed at one or more corners of the substrate, the at least one stress relief structure being adjacent to at least one die.
An aspect of this description relates to a method. The method includes bonding a first die to a substrate. The method further includes bonding a second die to the substrate. The method further includes adhering a first stress relief structure to the substrate, wherein a distance between the first stress relief structure to the first die is a first distance. The method further includes adhering a second stress relief structure to the substrate after adhering the first stress relief structure to the substrate, wherein a distance between the second stress relief structure is the first distance. In some embodiments, the method further includes curing an adhesive following adhering the first stress relief structure and the second stress relief structure to the substrate. In some embodiments, adhering the first stress relief structure to the substrate includes using an adhesive having a thermal conductivity greater than about 10 watts per meter Celsius (w/m-C). In some embodiments, adhering the second stress relief structure to the substrate includes adhering the second stress relief structure having a different composition from the first stress relief structure. In some embodiments, bonding the first die to the substrate includes using flip-chip bonding. In some embodiments, bonding the first die to the substrate includes using wire bonding. In some embodiments, adhering the first stress relief structure to the substrate includes adhering the first stress relief structure along a single side of the substrate. In some embodiments, adhering the second stress relief structure to the substrate includes adhering the second stress relief structure to a corner of the substrate.
An aspect of this description relates to a method. The method includes bonding a plurality of dies to a substrate. The method further includes adhering a first plurality of stress relief structures along a periphery of the substrate, wherein a distance between a first die of the plurality of dies and a first stress relief structure of the first plurality of stress relief structures is a first distance, and a distance between a second die of the plurality of dies and a second stress relief structure of the first plurality of stress relief structures is the first distance. In some embodiments, adhering the first plurality of stress relief structures comprises adhering the first stress relief structure along multiple edges of the substrate. In some embodiments, adhering the first plurality of stress relief structures comprises adhering the second stress relief structure along a single edge of the substrate. In some embodiments, bonding the plurality of dies to the substrate comprises bonding the first die having a first size to the substrate and bonding the second die having a second size, different from the first size, to the substrate. In some embodiments, bonding the plurality of dies to the substrate comprises bonding each die of the plurality of dies to the substrate without any stress relief structures between adjacent dies of the plurality of dies. In some embodiments, the method further includes adhering a second plurality of stress relief structures to the substrate. In some embodiments, adhering the second plurality of stress relief structures to the substrate comprises adhering at least one of the second plurality of stress relief structures to the substrate between the first die and the second die.
An aspect of this description relates to a method. The method includes bonding a plurality of dies to a substrate. The method further includes adhering a first stress relief structure along an entirety of a periphery of the substrate. The method further includes adhering a plurality of second stress relief structures along a periphery of the substrate, wherein a second stress relief structure of the plurality of second stress relief structures is between adjacent dies of the plurality of dies, and a third stress relief structure of the plurality of second stress relief structures is between a first die of the plurality of dies and the first stress relief structure. In some embodiments, adhering the plurality of second stress relief structures to the substrate comprises adhering the second stress relief structure along two sides of the first die. In some embodiments, adhering the plurality of second stress relief structures to the substrate comprises adhering the third stress relief structure along two sides of the first die. In some embodiments, adhering the plurality of second stress relief structures to the substrate comprises adhering the second stress relief structure along two sides of the first die and along two sides of a second die of the plurality of dies. In some embodiments, bonding the plurality of dies to the substrate comprises bonding the first die having a first size to the substrate and bonding a second die of the plurality of dies having a second size, different from the first size, to the substrate.
In the preceding detailed description, specific exemplary embodiments have been described. It will, however, be apparent to a person of ordinary skill in the art that various modifications, structures, processes, and changes may be made thereto without departing from the broader spirit and scope of the present disclosure. The specification and drawings are, accordingly, to be regarded as illustrative and not restrictive. It is understood that embodiments of the present disclosure are capable of using various other combinations and environments and are capable of changes or modifications within the scope of the claims.
The present application is a divisional of U.S. application Ser. No. 17/320,721, filed May 14, 2021, which is a continuation of U.S. application Ser. No. 16/728,305, filed Dec. 27, 2019, now U.S. Pat. No. 11,037,887, issued Jun. 15, 2021, which is a continuation of U.S. application Ser. No. 15/810,602, filed Nov. 13, 2017, now U.S. Pat. No. 10,522,477, issued Dec. 31, 2019, which is a continuation of U.S. application Ser. No. 15/062,570, filed Mar. 7, 2016, now U.S. Pat. No. 9,818,700, issued Nov. 14, 2017, which is a divisional of U.S. application Ser. No. 13/673,703, filed Nov. 9, 2012, now U.S. Pat. No. 9,312,193, issued Apr. 12, 2016, which are incorporated herein by reference in their entireties.
Number | Date | Country | |
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Parent | 17320721 | May 2021 | US |
Child | 18790785 | US | |
Parent | 13673703 | Nov 2012 | US |
Child | 15062570 | US |
Number | Date | Country | |
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Parent | 16728305 | Dec 2019 | US |
Child | 17320721 | US | |
Parent | 15810602 | Nov 2017 | US |
Child | 16728305 | US | |
Parent | 15062570 | Mar 2016 | US |
Child | 15810602 | US |